GB626044A - Improvements in or relating to gas turbine power plants - Google Patents
Improvements in or relating to gas turbine power plantsInfo
- Publication number
- GB626044A GB626044A GB15879/45A GB1587945A GB626044A GB 626044 A GB626044 A GB 626044A GB 15879/45 A GB15879/45 A GB 15879/45A GB 1587945 A GB1587945 A GB 1587945A GB 626044 A GB626044 A GB 626044A
- Authority
- GB
- United Kingdom
- Prior art keywords
- conduits
- air
- stage
- volute
- compressor
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/425—Combustion chambers comprising a tangential or helicoidal arrangement of the flame tubes
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB271480X | 1945-06-21 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB626044A true GB626044A (en) | 1949-07-08 |
Family
ID=10254985
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB15879/45A Expired GB626044A (en) | 1945-06-21 | 1945-06-21 | Improvements in or relating to gas turbine power plants |
Country Status (3)
Country | Link |
---|---|
US (1) | US2567079A (de) |
CH (1) | CH271480A (de) |
GB (1) | GB626044A (de) |
Families Citing this family (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2671315A (en) * | 1948-11-12 | 1954-03-09 | Rocheville Engineering Inc | Internal-combustion geared turbine |
US2809493A (en) * | 1951-03-19 | 1957-10-15 | American Mach & Foundry | Centrifugal flow compressor and gas turbine power plant with a centrifugal flow compressor, toroidal combustion chamber, and centripetal flow turbine |
US2808226A (en) * | 1952-02-08 | 1957-10-01 | Ryan Aeronautical Co | Turbine nozzle box |
US2928239A (en) * | 1954-03-16 | 1960-03-15 | Arthur W Goldstein | Impelled charge gas explosion turbine with constant volume, pressure raising combustion chambers |
US2888803A (en) * | 1954-08-30 | 1959-06-02 | Pon Lemuel | Intermittent combustion turbine engine |
US3010281A (en) * | 1957-12-24 | 1961-11-28 | Adolph J Cervenka | Toroidal combustion chamber |
US4186554A (en) * | 1975-11-10 | 1980-02-05 | Possell Clarence R | Power producing constant speed turbine |
US4081957A (en) * | 1976-05-03 | 1978-04-04 | United Technologies Corporation | Premixed combustor |
DE69127683D1 (de) * | 1990-12-20 | 1997-10-23 | Honda Motor Co Ltd | Gasgenerator für eine Gasturbine |
US5946902A (en) * | 1997-10-01 | 1999-09-07 | Siemens Aktiengesellschaft | Gas turbine engine with tilted burners |
EP1288441A1 (de) * | 2001-09-03 | 2003-03-05 | Siemens Aktiengesellschaft | Übergangsabschnitt einer Gasturbinenbrennkammer |
EP1722069A1 (de) * | 2005-05-13 | 2006-11-15 | Siemens Aktiengesellschaft | Gasturbine |
US7721547B2 (en) * | 2005-06-27 | 2010-05-25 | Siemens Energy, Inc. | Combustion transition duct providing stage 1 tangential turning for turbine engines |
EP1903184B1 (de) * | 2006-09-21 | 2019-05-01 | Siemens Energy, Inc. | Subsystem einer Verbrennungsturbine mit verwundenem Übergangskanal |
US8113003B2 (en) * | 2008-08-12 | 2012-02-14 | Siemens Energy, Inc. | Transition with a linear flow path for use in a gas turbine engine |
US8091365B2 (en) * | 2008-08-12 | 2012-01-10 | Siemens Energy, Inc. | Canted outlet for transition in a gas turbine engine |
US8276389B2 (en) * | 2008-09-29 | 2012-10-02 | Siemens Energy, Inc. | Assembly for directing combustion gas |
US8230688B2 (en) * | 2008-09-29 | 2012-07-31 | Siemens Energy, Inc. | Modular transvane assembly |
US8302377B2 (en) * | 2009-01-30 | 2012-11-06 | General Electric Company | Ground-based simple cycle pulse detonation combustor based hybrid engine for power generation |
US10012098B2 (en) * | 2012-02-29 | 2018-07-03 | Siemens Energy, Inc. | Mid-section of a can-annular gas turbine engine to introduce a radial velocity component into an air flow discharged from a compressor of the mid-section |
US9476355B2 (en) * | 2012-02-29 | 2016-10-25 | Siemens Energy, Inc. | Mid-section of a can-annular gas turbine engine with a radial air flow discharged from the compressor section |
US20130239585A1 (en) * | 2012-03-14 | 2013-09-19 | Jay A. Morrison | Tangential flow duct with full annular exit component |
US9021783B2 (en) * | 2012-10-12 | 2015-05-05 | United Technologies Corporation | Pulse detonation engine having a scroll ejector attenuator |
US9546601B2 (en) * | 2012-11-20 | 2017-01-17 | General Electric Company | Clocked combustor can array |
US9322335B2 (en) | 2013-03-15 | 2016-04-26 | Siemens Energy, Inc. | Gas turbine combustor exit piece with hinged connections |
US9810434B2 (en) * | 2016-01-21 | 2017-11-07 | Siemens Energy, Inc. | Transition duct system with arcuate ceramic liner for delivering hot-temperature gases in a combustion turbine engine |
CN105953266B (zh) * | 2016-05-04 | 2018-08-10 | 中国科学院工程热物理研究所 | 一种斜流燃烧室结构 |
GB201618016D0 (en) | 2016-10-25 | 2016-12-07 | Jiang Kyle | Gas turbine engine |
DE102019204544A1 (de) * | 2019-04-01 | 2020-10-01 | Siemens Aktiengesellschaft | Rohrbrennkammersystem und Gasturbinenanlage mit einem solchen Rohrbrennkammersystem |
US11885349B1 (en) * | 2022-08-18 | 2024-01-30 | Pratt & Whitney Canada Corp. | Compressor having a dual-impeller |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2504181A (en) * | 1950-04-18 | Double compound independent rotor | ||
US948292A (en) * | 1905-05-08 | 1910-02-01 | Platt Iron Works Co | Multistage centrifugal pump. |
US1218223A (en) * | 1913-08-07 | 1917-03-06 | Rateau Battu Smoot Company | Centrifugal blower. |
US1392090A (en) * | 1920-06-23 | 1921-09-27 | Tamini Mario | Rotary pump |
US2135939A (en) * | 1932-12-08 | 1938-11-08 | H B Motor Corp | Differential pressure mechanism |
US2056198A (en) * | 1934-08-18 | 1936-10-06 | Robert E Lasley | Power plant |
US2404334A (en) * | 1939-12-09 | 1946-07-16 | Power Jets Res & Dev Ltd | Aircraft propulsion system and power unit |
US2399046A (en) * | 1940-03-26 | 1946-04-23 | Gen Electric | Gas turbine power plant |
US2473356A (en) * | 1942-04-18 | 1949-06-14 | Turbo Engineering Corp | Combustion gas turbine arrangement |
US2400714A (en) * | 1942-06-11 | 1946-05-21 | Rowledge Arthur John | Jet propulsion power unit |
-
1945
- 1945-06-21 GB GB15879/45A patent/GB626044A/en not_active Expired
-
1946
- 1946-06-18 US US677496A patent/US2567079A/en not_active Expired - Lifetime
- 1946-06-24 CH CH271480D patent/CH271480A/de unknown
Also Published As
Publication number | Publication date |
---|---|
CH271480A (de) | 1950-10-31 |
US2567079A (en) | 1951-09-04 |
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